2014
DOI: 10.5028/jatm.v6i4.382
|View full text |Cite
|
Sign up to set email alerts
|

Experimental Investigation of a Monopropellant Thruster Using Nitrous Oxide

Abstract: Nitrous oxide is a monopropellant with potential for use in propulsion systems for orbit correction, positioning and attitude control of satellites. This paper presents experimental results with a 2N thruster prototype employing nitrous oxide gas decomposed by a rhodium oxide catalyst supported on alumina. Initially, the thruster design, the test bench and test procedures are described. Then the main experimental results, including thrust curves, mass flow rates, pressures and temperatures along the thruster a… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1

Citation Types

0
1
0

Year Published

2022
2022
2024
2024

Publication Types

Select...
5
1

Relationship

0
6

Authors

Journals

citations
Cited by 15 publications
(1 citation statement)
references
References 18 publications
(24 reference statements)
0
1
0
Order By: Relevance
“…To obtain heat flux used in Eqs. ( 2), ( 3), (6), and (9) this term is multiplied by the whole inner surface for SNE and the part of inner surface in contact with the bottom part of the fluid for PIM. The model constants C sf and n are assumed to be 0.01 and 1, respectively.…”
Section: X(p H) =mentioning
confidence: 99%
“…To obtain heat flux used in Eqs. ( 2), ( 3), (6), and (9) this term is multiplied by the whole inner surface for SNE and the part of inner surface in contact with the bottom part of the fluid for PIM. The model constants C sf and n are assumed to be 0.01 and 1, respectively.…”
Section: X(p H) =mentioning
confidence: 99%